View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 59234U 26145.45547558 +.00000000 +00000-0 +64971-5 0 00009
2 59234 43.0014 58.9987 0000710 269.1673 90.9097 15.27573381 01
| Epoch (UTC): | 25 May 2026 10:55:53 |
| Eccentricity: | 0.0000710 |
| inclination: | 43.0014° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 58.9987° |
| argument of perigee: | 269.1673° |
| revolutions per day: | 15.27573381 |
| mean anomaly at epoch: | 90.9097° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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